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(11) | EP 2 169 313 A3 |
| (12) | EUROPEAN PATENT APPLICATION |
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| (54) | Fuel Lance for a Gas Turbine Engine |
| (57) The invention relates to a fuel lance (7) for introducing fuel into a gas flow in
a combustor (1) of a gas turbine engine, whereby a region of the lance (7) through
which the fuel is introduced into the gas flow comprises a generally helical formation
(12).
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